A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Home Built
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

compound curves in plywood



 
 
Thread Tools Display Modes
  #1  
Old April 12th 05, 07:44 PM
BA-100
external usenet poster
 
Posts: n/a
Default

UltraJohn
thlink.net:



I'm pretty sure that the process would be to heavy for the strength
it would provide, unless it were modified to provide several very
thin crossing layers, all of which woul have to be tightly glued to
each other


I'm no expert in (or any field) but several people have mentioned
about the lack of strength a single layer plywood would have and you'd
need several layers (ad various angles) etc etc. Yet the most common
new "core" constructions uses styrofoam for a core, I'd think the
plywood at almost any thickness would be stronger. The reason for use
the plywood would be for the looks (at least that's my guess).


Well, ultimately the wood would be for looks. I could easily make a strong
fuse for this using plywood. While i was at it I could clean up the
aerodynamics and use carbon fibre for the wing spars. The added strength
would enable a longer, thinner wing and I could probably delete the struts
into the bargain! Thing is, it wouldn't be a Baby Albatross anymore. Ithink
you're confused about what is meant by single layer. A single layer
wouldn't be plywood, it'd be one layer of a sheet of plywood. It' be a ply
after layers were glued together. I can't see foam being used succesfully
as a core in this design either. Either I have to use the built up scarfed
panels method or figure a way to make a thin plywood teardrop with a farily
tight radius. Seems possible to make a three or four ply lamination using
single veneers set at angles to each other wrapping four inch or so veneer
strips over a male mold one at a time and trimming to match it's neighbor.
  #2  
Old April 13th 05, 03:21 AM
COLIN LAMB
external usenet poster
 
Posts: n/a
Default

The greatness of the Wright Brothers was that they were not limited by what
they did not know.

The Bowlus was a unique approach to flight, The design lends itself to
learning skills to make a modern replacement using either rekindled or
entirely new process.

Colin


  #3  
Old April 13th 05, 05:29 AM
BA-100
external usenet poster
 
Posts: n/a
Default

"COLIN LAMB"
thlink.net:

The greatness of the Wright Brothers was that they were not limited by
what they did not know.

The Bowlus was a unique approach to flight, The design lends itself
to learning skills to make a modern replacement using either rekindled
or entirely new process.


True, vbut it wasn't exactly groundbreaking technology in 1938, either. A
modern replacement's been done. I want a fairly close replica.. When i
talked to Steven DuPont abou tit, he said "What do you want to build a
piece of **** like that for? I'm building an HP18! Build one of those."



 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
Nut/thread securing compound nauga Home Built 7 April 22nd 04 07:56 AM
Randolph Wing Walk Compound Larryskydives Owning 7 March 7th 04 09:44 PM
Plywood Kathi Jo Home Built 3 January 12th 04 10:48 PM
Somebody Terrified of Compound Curves ---- Or Just Lazy Larry Smith Home Built 8 October 31st 03 02:40 PM
Substitute for Mahogany plywood Kelvin & Janice Rempel Home Built 1 September 5th 03 08:02 PM


All times are GMT +1. The time now is 06:23 PM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.